Cessna T182T Operating Manual
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Cessna T182T Operating Manual

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Cessna T182T Aircraft Operating Manual

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Summary of Contents for Cessna T182T

  • Page 1 Cessna T182T Aircraft Operating Manual...

  • Page 2: Table Of Contents

    Contents Introduction ..............................4 182T Operational Limitations ........................5 Airspeed Limitations ........................5 Airspeed Indicator Markings .......................5 Powerplant Limitations.......................6 Weight Limits ..........................7 Centre of Gravity Limits ......................8 Maneuver Limits.........................8 Flight Load Factor Limits ......................8 Fuel Limitations ..........................8 Maximum Operating Altitude .....................8 Flap Limitations ..........................8 Autopilot Limitations ........................9 Airport Runway Limitations ......................9...
  • Page 3 Amplified Normal Procedures.........................26 Cross Country Operations ........................36 Airspeed for Emergency Operation ...................39 Amplified Emergency Procedures......................45 Cross Country Emergency Procedures......................49...

  • Page 4: Introduction

    This Aircraft Operating Manual is a summary of key aspects of the Pilot’s Operating Handbook. It is not meant to be a replacement for the POH but rather a summary of key aspects of the Cessna T182T and an outline of the training requirements that the Calgary Flying Club will follow for pilots wishing to get...

  • Page 5: 182T Operational Limitations

    This section includes aircraft limitations from the POH as well as CFC limitations for the operation of CFC T182T aircraft. It is the responsibility of the Pilot-in-Command to ensure that the aircraft is operated in accordance with the limitations in this section as well as the POH of the aircraft.

  • Page 6: Powerplant Limitations

    Aviation Grade 100LL (Blue) Minimum Fuel Quantity: Minimum fuel required for the flight + 45 mins OR 46 U.S. Gallons – Whichever is greater. Oil Grade  All CFC T182T aircraft must use SAE 15W50 oil.  Minimum Oil Quantity is 5 QT.

  • Page 7: Weight Limits

    Propeller  McCauley Propeller Systems B3D36C442-C/80VSB-1.  Propeller Diameter: 79 inches  Propeller Blade Angle at 30-inch station: o Low: 15.3° o High: 35.4° Powerplant Instrument Markings: Weight Limits...

  • Page 8: Centre Of Gravity Limits

    Centre of Gravity Limits Maneuver Limits Flight Load Factor Limits Fuel Limitations Minimum Fuel Quantity: 46 U.S. Gal OR Fuel required for flight + 45 min, whichever is greater Maximum Operating Altitude Certified Maximum Operating Altitude: 20 000 ft Flap Limitations ...

  • Page 9: Autopilot Limitations

    A runway is considered contaminated when 25% or more of the required length and width of the runway is contaminated. CFC T182T aircraft are permitted to take off and land on Dry, Wet and Trace contaminated runways. Trace contamination refers to any contaminant with a depth of 1/8in (0.13 in) or less.

  • Page 10: Standard Call-Outs

    Standard Call-Outs Phase of Flight Call-Outs Autopilot engage “AUTOPILOT ON” Autopilot disengaged “AUTOPILOT DISENGAGED” Approaching transition altitude/flight level “TRANSITION ____ SET” Altitude Change “ ____ FEET SET ” OR “____ ALT ARM “ (If AP is engaged) 1000 Feet above/below desired Altitude “16000 FOR 17000”...

  • Page 11: 182T Training Syllabus

    182T Training Syllabus Minimum Requirements for Rental Day VFR Below 10,00ft:   100 Hours Total Time  25 hours PIC X-Country Post PPL – Destinations outside of 100nm Radius Day VFR Above 10,000ft:   150 Hours Total Time ...

  • Page 12: Air Lesson Plans

    Air Lesson Plans The following lesson plans will cover the major differences in airframe, performance, procedures, equipment, capabilities and operation of the Calgary Flying Club’s Cessna T182T. What’s Different about the T182T? How is the Cessna T182T different from the Cessna 172s? ...

  • Page 13: Lesson Plan 1: Basic Aircraft Familiarization (Ground)

    Lesson Plan 1: Basic Aircraft Familiarization (Ground) Estimated Duration: 6 Hours Note: This could be done as a one-day session or as two individual sessions Aim: To familiarize participants with the aircraft and its equipment. Particularly with respect to limitations, speeds, procedures, systems and equipment that are different from those C172 aircraft.

  • Page 14: Lesson Plan 2: Basic Aircraft, Engine And Avionics Handling (Air)

    Lesson Plan 2: Basic Aircraft, Engine and Avionics Handling (Air) Estimated Duration: 3 Hours Note: May be combined with LP3 if sufficient prior experience, and aircraft 1 Hour Ground, 2 Hours Air handling gives evidence of this. Aim: To familiarize the participant with the basic procedures for operation of the aircraft Flight Route/Area: Cremona area, then Sundre Airport ...

  • Page 15: Lesson Plan 3: Aircraft Emergencies, Specialty Takeoffs And Landings (Air)

    Lesson Plan 3: Aircraft Emergencies, Specialty Takeoffs and Landings (Air) Estimated Duration: 4 Hours Note: May be combined with LP3 if sufficient prior experience, and aircraft 1 Hour Ground, 1 Hours Sim, 2 handling gives evidence of this. Hours Air Aim: To familiarize the participant with emergency procedures, specialty takeoffs and landings and basic use of autopilot Flight Route/Area: Longview area, then High river Airport...

  • Page 16: Lesson Plan 4: Cross-Country Day Vfr Below 10 000 Ft (Air)

    Lesson Plan 4: Cross-Country Day VFR below 10 000 ft (Air) Estimated Duration: 4.5 Hours Note: Advanced Operations 1.5 Hour Ground, 1hour Sim, 2 Hours Air Aim: To prepare the participant for day VFR non-mountain cross-country flights below 10 000 ft Flight Route/Area: Springbank Airport –...

  • Page 17: Lesson Plan 5: Cross-Country Night Vfr Below 10 000 Ft (Air)

    Lesson Plan 5: Cross-Country Night VFR below 10 000 ft (Air) Estimated Duration: 4 Hours Note: Advanced Operations 1 Hour Ground, 1 hour Sim, 2 Hours Air Aim: To prepare the participant for night VFR non-mountain cross-country flights below 10 000 ft Flight Route/Area: Springbank –...

  • Page 18: Lesson Plan 6: Cross-Country Vfr Above 10 000 Ft (Air)

    Lesson Plan 6: Cross-Country VFR above 10 000 ft (Air) Estimated Duration: 4 Hours Note: Advanced Operations 2 Hour Ground, 1 hour Sim, 3 Hours Air Aim: To prepare the participant for VFR cross-country flights above 10,000 feet, including mountainous areas Flight Route/Area: Springbank–Golden (VFR at 12,000’) Golden–Revelstoke (VFR below peak tops)
  • Page 19  Review point to come off oxygen, and how to shut oxygen system off  Monitor proper communications and procedures into Golden  Monitoring proper aircraft handling for descent, approach and landing  Monitor proper takeoff and departure procedures out of Golden, including communication and ETA update with Pacific Radio ...

  • Page 20: Lesson Plan 7: Cross-Country Ifr Below And Above 10 000 Ft (Ground)

    Lesson Plan 7: Cross-Country IFR Below and Above 10 000 ft (Ground) Estimated Duration: 4 Hours Note: Advanced Operations 3 Hour Ground, 1 Hours SIM Aim: To familiarize the participant with the features and usage of the GTN 750Xi for IFR flight. To familiarize the participant with the use of the autopilot for IFR procedures.

  • Page 21: Lesson Plan 8: Cross-Country Ifr Below And Above 10 000 Ft (Air)

    Lesson Plan 8: Cross-Country IFR Below and Above 10 000 ft (Air) Estimated Duration: 4 Hours Note: Advanced Operations 1 Hour Ground, 3 Hours Air Aim: To prepare the participant for IFR cross-country flights at up to FL180 Pre-requisites: Lesson Plans 7 completed & a valid IFR rating Flight Route/Area: 1.
  • Page 22   Monitor point to come off Land Cranbrook for short break, oxygen, and how to shut oxygen update flight plan, review weather, system off confirm no icing, review departure  procedure and comm failure Monitor power plant management at FL190 procedure, confirm alternate still good, review Class A airspace ...

  • Page 23: Recurrent Training

    Recurrent Training Recurrent training is completed once a year and is dependant on the type of checkout the member is seeking. VFR Below 10,000ft Day or Night  Lesson Plan 4 or 5 may be completed as part of the recurrent training dependant on Day or Night check.

  • Page 24: 182T Normal Procedures

    182T Normal Procedures After Start Normal Checklist Transponder ……………………………………..…………. STBY ATIS ………………………………………………….…….……COPY Pre-Flight Inspection Altimeter ………………………………………….……….….. SET Flight Instruments ………………..……………….…….… SET Know Amplified Procedures Nav Instruments …………………………………….……… SET Fire Extinguisher Fuel ……………………………………………………………. BOTH Seat Belts Brakes ………………………………………………..…….. CHECK No Smoking First Aid Kit Run Up Survival Equipment...
  • Page 25 After Landing Take Off – Normal Radio …………………………………………… GROUND FREQ Power ………………………………. 32” Hg and 2400 RPM Flaps ………………………………………………………………. UP Mixture ……………………………….………………….. 24 GPH Cowl Flaps ……………………………….………………… OPEN Rotate …………………………………………..………... 60 KIAS Transponder ………………………………….……………. STBY Climb ………………………….….. 70KIAS (20); 80 KIAS (0) Timer ………………………………………………….……..

  • Page 26: Amplified Normal Procedures

    Amplified Normal Procedures Pre-Flight Inspection CABIN 1. Pitot Tube Cover – Remove and check pitot tube for blockage 2. Parking Brake – Set 3. Control Wheel Lock – Remove 4. Ignition Switch – OFF 5. Avionics Master Switch – OFF 6.
  • Page 27 2. Flap – Check for security and condition RIGHT WING 1. Wing Tie -Down – Disconnect 2. Fuel Tank Vent Opening – Check for blockage 3. Main Wheel Tire – Check for proper inflation and general condition (weather check, tread depth and wear) 4.
  • Page 28 Amplified Pre-Flight Inspection  Flight controls and trim tab should be checked for free and correct movement and security  Security of all inspection plates should be checked following periodic inspections  Check external static pressure source hole for stoppage ...
  • Page 29 12. Flashing Beacon and Navigation Lights – ON as required 13. Avionics Master Switch – ON 14. Radios – ON 15. Flaps – RETRACT STARTING ENGINE (WITH External Power) 1. Throttle – OPEN ¼” 2. Propeller – HIGH RPM 3. Mixture – IDLE CUT OFF 4.
  • Page 30 o Crank starter for 10 sec followed by 20 sec cool down; Repeat two additional times followed by 10 min cool down period before trying again; Crank starter again, 3 cycles of 10 sec each, followed by 20 seconds of cool down. If engine fails to start, an investigation to determine the cause is needed BEFORE TAKEOFF 1.
  • Page 31 Alternator Check  Positive verification can be made by loading the electrical system momentarily (3-5 sec) with the landing light or by operating the wing flaps during the engine run up  Ammeter will remain within a needle width of its initial reading if the alternator and alternator control unit are operating properly Elevator Trim ...
  • Page 32 Crosswind Takeoff  Under strong x-wind conditions minimum flap setting necessary for the field length, to minimize drift angle immediately after take off  With ailerons into the wind the aircraft is accelerated to a slightly higher than normal speed and pulled briskly off to prevent possible settling back to the runway while drifting Enroute Climb ...
  • Page 33  Cruise performance data in handbook is based on a recommended lean mixture setting which may be established using the T.I.T indicator at powers of 88% MCP and below as follows: 1. Lean the mixture slowly until the T.I.T peaks and begins to drop or until reaching the T.I.T red line 2.
  • Page 34 LANDING NORMAL LANDING 1. Airspeed – 70-80 KIAS (flaps UP) 2. Wing Flaps – As Desired a. Below 140 KIAS – 0° to 10° b. Below 120 KIAS – 10° to 20° c. Below 100 KIAS – 20° to FULL 3.
  • Page 35 COLD WEATHER OPERATION  The waste gate controller will not respond quickly to variations in manifold pressure when oil temperature is near the lower limit of the green arc. Therefore, under these conditions, throttle motion should be made slowly and care should be exercised to prevent exceeding the 32” Hg manifold pressure limit.

  • Page 36: Cross Country Operations

    Cross Country Operations C182T Turbocharged Engine Operations Takeoff Takeoff power set to 32 in MP, 2400 RPM and Mixture at 24 gph. Manifold Pressure MP and Fuel Flow FF needles (same gauge – under the turn coordinator) should both be pointing to near the red line. RPM (under the VSI) should be near red line.
  • Page 37 to start reducing from 24” cruise power four minutes before that, or about 35 miles away from the airport. Enrichen mixture ½ turn every 1000’ descent NOTE: During all phases of flight, cylinder head temperatures and T.I.T. should be monitored. Use of cowl flaps, power and mixture settings should be determined in consideration of cylinder head temperatures and T.I.T.
  • Page 38 Weather Requirements Flights conducted under IFR must be completed in accordance with an IFR clearance. Flights conducted under VFR must be conducted in VMC at all times and under Controlled VFR. If unable to comply with the above requirements:  The aircraft must be operated in VMC at all times.

  • Page 39: Airspeed For Emergency Operation

    Airspeed for Emergency Operation Engine Failure After Takeoff Wing Flaps Up 75 KIAS Wing Flaps Down 70 KIAS Maneuvering Speed 3100 lbs 110 KIAS 2600 lbs 101 KIAS 2100 lbs 91 KIAS Maximum Glide 3100 lbs 75 KIAS 2600 lbs 69 KIAS 2100 lbs 62 KIAS...
  • Page 40 ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed – 75 KIAS (Best Glide Speed) 2. Fuel Selector Valve – BOTH 3. Auxiliary Fuel Pump Switch – ON 4. Mixture – RICH (if restart does not occur) 5. Ignition Switch – BOTH (or START, if propeller is stopped) NOTE If propeller is windmilling, engine will restart automatically within a few seconds, If propeller has stopped (possible at low speeds), turn ignition switch to START, advance throttle slowly from idle, and lean the...
  • Page 41 DITCHING 1. Radio – TRANSMIT MAYDAY on 121.5, giving location and intentions and SQUAWK 7700 (If installed) 2. Heavy Objects (in baggage area) – SECURE OR JETTISON (If possible) 3. Passenger Seat Back – MOST UPRIGHT POSITION 4. Seats and Seat Belts – SECURE 5.
  • Page 42 ENGINE FIRE IN FLIGHT 1. Mixture – IDLE CUT OFF 2. Fuel Selector Valve – PUSH DOWN AND ROTATE TO OFF 3. Auxiliary Fuel Pump Switch – OFF 4. Master Switch – OFF 5. Cabin Heat and Air – OFF (except overhead vents) 6.
  • Page 43 WING FIRE 1. Landing/Taxi Light Switches – OFF 2. Navigation Light Switch – OFF 3. Strobe Light Switch – OFF 4. Pitot Heat Switch – OFF NOTE Perform a sideslip to keep the flames away from the fuel tank and cabin. Land as soon as possible using flaps only as required for final approach and touchdown ICING 1.
  • Page 44 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS AMMETER SHOWS EXCESSIVE RATE OF CHARGE (Full Scale Deflection) 1. Alternator – OFF !CAUTION! WITH THE ALTERNATOR SIDE OF THE MASTER SWITCH OFF, COMPASS DEVIATIONS OF AS MUCH AS 25 DEGREES MAY OCCUR 2. Nonessential Electrical Equipment – OFF 3.

  • Page 45: Amplified Emergency Procedures

    Amplified Emergency Procedures Engine Failure  If occurs on take off roll STOP on the remaining runway  If airborne prompt lowering of the nose to maintain airspeed and establish a glide attitude is the first response. LAND STRAIGHT AHEAD with only small changes in direction to avoid obstructions ...
  • Page 46 o Check accuracy of the turn by observing the compass heading which should be reciprocal of the original o If necessary, adjust heading primarily with skidding motions rather than rolling motions so compass is more accurate o Maintain altitude and airspeed by cautious application of elevator control. Avoid over controlling by keeping the hands off the control wheel as much as possible and steering only with rudder Emergency Descent Through Clouds...
  • Page 47 Static Source Blocked  If erroneous readings of the static source instruments (airspeed, altimeter and VSI) are suspected pull the alternate source valve  With this pulled refer to the alternate static source airspeed calibration table in section 5  Maximum airspeed and altimeter variation from normal are 5 knots and 50 feet over the normal operating range with a window(s) closed.
  • Page 48 Low Oil Pressure  If low oil pressure annunciator (OIL PRESS) illuminates, check oil pressure gauge to confirm low oil pressure condition  If oil pressure and oil temp remain normal, it is possible the oil pressure sending until or relief valve is malfunctioning ...

  • Page 49: Cross Country Emergency Procedures

    Cross Country Emergency Procedures Weather Deviations Thunderstorms Note As per POH Supplement 23, the WX-500 Stormscope is approved for use only in avoiding hazardous weather (thunderstorms); use of the WX-500 to penetrate hazardous weather is prohibited. 1. Stormscope…CONFIRM ON Note A yellow lightning bolt on a light blue background signifies that Stormscope data is being displayed.
  • Page 50 Endurance + Takeoff Time = Fuel Exhaustion Time Fuel Exhaustion Time less ETA at Alternate = Fuel at Alternate Note Fuel required to divert to an alternate aerodrome as well as applicable reserves and contingencies should be calculated.  Fuel…CHECK Note It is recommended to determine fuel utilized and reassess the current fuel situation and compare it against the fuel required to divert as well as applicable reserves and contingencies.
  • Page 51 If Emergency Descent is required: **Suggested procedure given general practice in absence of published procedure** 1. Safe Altitude…DETERMINE Note Selected safe altitude to descend to should be 10,000ASL or the minimum altitude that would permit safe flight with respect to weather and terrain avoidance (whichever is greater) 2.
  • Page 52 Inadvertent Icing Encounters Note This aircraft is not certified for flight into known icing conditions. As per POH Supplement 17, installation of Propeller Heat does not change the limitations of the aircraft. 1. Master Switch…ON 2. Propeller Heat…ON 3. Propeller Heat…CHECK GREEN PROP HEAT LIGHT ILLUMINATED 4.
  • Page 53 *Approach at 80 to 90 KIAS depending upon the amount of the ice accumulation. 14. Landing Attitude…LEVEL *Perform a landing in a level attitude Missed approaches should be avoided whenever possible because of severely reduced climb capability. Static Source Blockage (Erroneous Instrument Reading Suspected) 1.

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